# Service difficulty reports: N254PS, cancelled Dec 9, 2025

A list on [N254PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N254PS-2025-12-09.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 92 reports

- [SDR VNAA2020030611101](https://openairdocs.org/sdr/VNAA2020030611101.md): Unknown · malfunctioned · Mar 4, 2020 · N254PS · Cndair CL6002B19 · Cabin Cooling System
  > R/H PACK FAIL IN FLIGHT WITH LH PACK ON DEFERRAL. PERFORMED OPS CHECK OF RH PACK IAW CRJ 200 AMM 21-51-00-710-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2020013021102](https://openairdocs.org/sdr/VNAA2020013021102.md): Control Unit · failed · Jan 27, 2020 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > JUST GETTING READY TO START APPROACH FOR CHA AT ABOUT 3000 FT. SET FLAPS TO 8 DEGREES AND GOT A FLAP FAIL CAUTION MESSAGE. CREW BROKE OFF APPROACH, RAN QRH, THEN MADE DECISION TO DIVERT TO TYS DUE TO RUNWAY LENGTH AND A WET RUNWAY. LANDED TYS WITHOUT INCIDENT.
- [SDR VNAA2018111211102](https://openairdocs.org/sdr/VNAA2018111211102.md): Strut · contaminated · Nov 12, 2018 · N254PS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD SERVICED NLG STRUT SUSPECTED AIR IN THE SYSTEM.
- [SDR VNAA2018102811102](https://openairdocs.org/sdr/VNAA2018102811102.md): Sensor · out of limits · Oct 28, 2018 · N254PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > THE CREW RECEIVED A NOSE GEAR DISAGREE AFTER TAKEOFF. THEY RAN THE QRH WHICH TOLD THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY RETURNED TO SHV AFTER BURNING OFF SOME FUEL. FOUND NGL WOW SENSOR TO BE OUT OF LIMITS. ADJUSTED SENSOR IAW CRJ200AMM. OPS CHEC
- [SDR VNAA2018102599915](https://openairdocs.org/sdr/VNAA2018102599915.md): Door Sill · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GALLEY SVC DOOR/LOWER SILL ANGLE CORRODED IN THREE LOCATIONS. C/A:. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER SILL ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-13 AND 51-42-21.
- [SDR VNAA2018102599914](https://openairdocs.org/sdr/VNAA2018102599914.md): Angle · cracked · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE FS625 OBLIQUE ANGLE IS CRACKED. C/A: REMOVED AND REPLACED RT OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-06.
- [SDR VNAA2018102599913](https://openairdocs.org/sdr/VNAA2018102599913.md): Floorbeam · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DISCREPANCY: CARGO FLOORBEAM IS CORRODED LT SIDE FS 589.00 BETWEEN LBL 9 AND LBL 18. CORRECTIVE ACTION: REMOVED CORROSION FROM FLOORBEAM CAP STRIP AND FOUND CAP STRIP TO BE OUT OF LIMITS, REMOVED AND REPLACED FLOORBEAM CAP STRIP IAW SRM 51-40-11 (TR51-42), 51-
- [SDR VNAA2018102599912](https://openairdocs.org/sdr/VNAA2018102599912.md): Floorbeam · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DISCREPANCY: LBL 27 FLOORBEAM IS CORRODED BETWEEN FS 589 - FS 605 CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM CAP IAW REO 601R-53-61-6742 REV -- DATED 2018/10/16.
- [SDR VNAA2018102599911](https://openairdocs.org/sdr/VNAA2018102599911.md): Seat Track · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: RBL9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559 TO FS 559+80. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK @ RBL 9 FS 559-55-+80 IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.
- [SDR VNAA2018102599910](https://openairdocs.org/sdr/VNAA2018102599910.md): Seat Track · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: LBL 9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559-FS559+80 CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.
- [SDR VNAA2018102599909](https://openairdocs.org/sdr/VNAA2018102599909.md): Bulkhead · cracked · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DISCREPANCY: FS621 REAR PRESSURE BULKHEAD WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA @ LBL 27 WL 106.25 TO WL 137.25 AT 50% FSH, FAILED NDT INSPECTION. CORRECTIVE ACTION: REPAIRED REAR PRESSURE BULKHEAD AT LBL 27 IAW REO'S 601R-5
- [SDR VNAA2018102599908](https://openairdocs.org/sdr/VNAA2018102599908.md): Strap · damaged · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > DISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, LEFT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2879 REV -- DATED 2018/10/16.
- [SDR VNAA2018102599907](https://openairdocs.org/sdr/VNAA2018102599907.md): Strap · damaged · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > DISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, RIGHT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2878 REV -- DATED 2018/10/16.
- [SDR VNAA2018102599906](https://openairdocs.org/sdr/VNAA2018102599906.md): Angle · cracked · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Cargo/Baggage Doors
  > DISCREPANCY: AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.
- [SDR VNAA2018102599905](https://openairdocs.org/sdr/VNAA2018102599905.md): Tie Down · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Cargo Compartments
  > DISCREPANCY: 5 CARGO TIE DOWNS ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED 5 EA ANCHOR PLATES IAW SRM 51-41-02.
- [SDR VNAA2018102599904](https://openairdocs.org/sdr/VNAA2018102599904.md): Cargo Track · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: RBL9 CARGO SEAT TRACK IS CORRODED AT FS 559+112. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL9 FS559+112 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.
- [SDR VNAA2018102599903](https://openairdocs.org/sdr/VNAA2018102599903.md): Cargo Track · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL18 FROM FS559+80 TO FS559+96. CORRECTIVE ACTION: REMOVED AND REPLACED CARGO SEAT TRACK AT LBL18 FROM FS559+80 TO FS559+96 IAW AMM 53-01-11-400-802.
- [SDR VNAA2018102599902](https://openairdocs.org/sdr/VNAA2018102599902.md): Cargo Track · corroded · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL9 BETWEEN FS559+80 AND 559+96. CORRECTIVE ACTION: REMOVED AT REPLACED CARGO SEAT TRACK AT LBL9 BTWN FS559+80 AND 559+96 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.
- [SDR VNAA2018102599901](https://openairdocs.org/sdr/VNAA2018102599901.md): Fitting · cracked · Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DISCREPANCY: RT INBOARD CLIP AT F.S. 484 IS CRACKED CORRECTIVE ACTION: REMOVED AND REPLACED 601R31171-9 CLIP IAW SRM 53-41-43 AND 51-42-21.
- [SDR VNAA2017090611101](https://openairdocs.org/sdr/VNAA2017090611101.md): Landing Gear · malfunctioned · Sep 6, 2017 · N254PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF, THE CREW TRIED TO RETRACT THE LANDING GEAR AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE MAIN GEAR DISPLAYED UP AND LOCKED, BUT THE NOSE GEAR WAS STILL SHOWING DOWN AND GREEN. FOLLOWED THE QRH AND SELECTED THE GEAR MANUAL RELEASE AND ALL
- [SDR VNAA2017040500005](https://openairdocs.org/sdr/VNAA2017040500005.md): Proximity Sensor · malfunctioned · Apr 5, 2017 · N254PS · Cndair CL6002B19 · Door Warning System
  > PASSENGER DOOR AMBER MESSAGE IN FLIGHT. REMOVED AND REPLACED PROXIMITY SENSOR PS9MB.
- [SDR VNAA2017022400031](https://openairdocs.org/sdr/VNAA2017022400031.md): Latch · sticking · Feb 24, 2017 · N254PS · Cndair CL6002B19 · Passenger/Crew Doors
  > CAN NOT LATCH MAIN CABIN DOOR. CLEANED AND LUBRICATED LATCH. OPERATIONAL CHECK GOOD.
- [SDR VNAA2017021400022](https://openairdocs.org/sdr/VNAA2017021400022.md): Switch · inoperative · Feb 14, 2017 · N254PS · Cndair CL6002B19 · Doors
  > CABIN ALTITUDE AND OVERBOARD COOL CAUTION MESSAGE IN FLIGHT. AIRCRAFT WAS NOT PRESSURIZING. REMOVED AND REPLACED PASSENGER DOOR SWITCH S102MB.
- [SDR VNAA2016101400046](https://openairdocs.org/sdr/VNAA2016101400046.md): Bulkhead · cracked · Oct 14, 2016 · N254PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION AT LBL27.50, WL130. MAINTENANCE REPAIRED BULKHEAD WEB AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016101400045](https://openairdocs.org/sdr/VNAA2016101400045.md): Strap · corroded · Oct 14, 2016 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP SIDE OF STRAP AT FS 559, LBL30. MAINTENANCE REMOVED AND REPLACED STRAP AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016101300016](https://openairdocs.org/sdr/VNAA2016101300016.md): Bulkhead Web · cracked · Oct 13, 2016 · N254PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 27.50 AT TOP OF CARGO DOOR AFT TRACK. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR VNAA2016101300015](https://openairdocs.org/sdr/VNAA2016101300015.md): Strap · corroded · Oct 13, 2016 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON TOP SIDE OF STRAP AT BS 559 NEAR LBL 30. MAINTENANCE REMOVED AND REPLACED STRAP IAW SRM.
- [SDR VNAA2016040800009](https://openairdocs.org/sdr/VNAA2016040800009.md): Warning Light · false activation · Apr 8, 2016 · N254PS · Cndair CL6002B19 · Steering Unit
  > CREW REPORTED A "STEERING INOPERATIVE" MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, COMPLIED WITH SYS RESET AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016011100009](https://openairdocs.org/sdr/VNAA2016011100009.md): Control Lever · failed · Jan 11, 2016 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL MESSAGE DURING CLIMBOUT. FLAPS AT 8 DEGREES DURING TAKEOFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW FIM, R & R FLAP LEVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015111100005](https://openairdocs.org/sdr/VNAA2015111100005.md): Flap System · malfunctioned · Nov 11, 2015 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAP FAIL AT 30 DEGREES ON FINAL APPROACH. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM AND DETERMINED SYS OPERATED NORMALLY AND THAT CAUSE OF DISCREPANCY WAS OPERATOR ERROR. MAINTENA
- [SDR VNAA2015072100023](https://openairdocs.org/sdr/VNAA2015072100023.md): Battery Pack · discharged · Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 3 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015072100022](https://openairdocs.org/sdr/VNAA2015072100022.md): Battery Pack · discharged · Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT HAD BEEN LT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 1 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015072100021](https://openairdocs.org/sdr/VNAA2015072100021.md): Battery Pack · discharged · Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015072100020](https://openairdocs.org/sdr/VNAA2015072100020.md): Battery Pack · discharged · Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015021700013](https://openairdocs.org/sdr/VNAA2015021700013.md): Smoke Detector · false activation · Feb 17, 2015 · N254PS · Cndair CL6002B19 · Smoke Detection
  > CREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT. ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LAV SMOKE DETECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015021700012](https://openairdocs.org/sdr/VNAA2015021700012.md): Coalescer Bag · odor · Feb 17, 2015 · N254PS · Cndair CL6002B19 · Humidity Control System
  > CREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT COALESCER BAG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015010600006](https://openairdocs.org/sdr/VNAA2015010600006.md): Adc · failed · Jan 6, 2015 · N254PS · Cndair CL6002B19 · Air Data Computer
  > CREW REPORTED CAPTAIN’S PRIMARY FLIGHT DISPLAY (PFD) LOST AIRSPEED, ALTITUDE AND NAVIGATION DATA IN FLIGHT. MACH TRIM ALSO DISCONNECTED AND AUTOPILOT DISENGAGED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT. R & R NR 1 AIR DATA
- [SDR VNAA201412020001](https://openairdocs.org/sdr/VNAA201412020001.md): Fuel Nozzle · leaking · Dec 2, 2014 · N254PS · Cndair CL6002B19 · APU Engine Fuel and Control
  > DURING START OF APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLSHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE/FUEL LINE CHAFED AND INDICATION OF FIRE. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014120200001](https://openairdocs.org/sdr/VNAA2014120200001.md): Line · chafed · Dec 2, 2014 · N254PS · Cndair CL6002B19 · APU Engine Fuel and Control
  > WHILE STARTING THE APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE AND NOZZLE FUEL LINE CHAFED. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014112600016](https://openairdocs.org/sdr/VNAA2014112600016.md): Door Sill · corroded · Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL IS CORRODED AROUND NUTPLATES BS 574 - 621. REMOVED AND REPLACED THE CORRODED DOOR SILL IAW REO 601-53-61-1574, REV B.
- [SDR VNAA2014112600015](https://openairdocs.org/sdr/VNAA2014112600015.md): Floorbeam · damaged · Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM HAS ELONGATED HOLE AST FS 559 + 34 ON OTBD SIDE WITH SCREW STILL STUCK IN HOLE. REPAIRED FLOORBEAM AT FS 559+34, RBL 9 IAW SRM 53-00-43, REV 32, REPAIR 1, FIGURE 203, SHEET 2.
- [SDR VNAA2014112600014](https://openairdocs.org/sdr/VNAA2014112600014.md): Stringer · cracked · Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED.750" LONG AT FS 379.00. REPAIRED CRACKED STRINGER 3L AT FS 379.0 IAW REO 601R-53-21-2582 AND SRM 53-00-03.
- [SDR VNAA2014112600013](https://openairdocs.org/sdr/VNAA2014112600013.md): Attach Fitting · damaged · Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PASSENGER DOOR ATTACHMENT STRUCTURE FOR STOP PANEL 832 ET FASTENER HOLE ENLARGED. REPAIRED DAMAGED NUTPLATE AND BOTTOM ROW OF PANEL 832 ET STEP STRUCTURE IAW EO NR CL600-2B19-52-L02946.
- [SDR VNAA201411170007](https://openairdocs.org/sdr/VNAA201411170007.md): Stiffener · cracked · Nov 26, 2014 · N254PS · Cndair CL6002B19 · Engine Air Intake System
  > THE RIGHT INLET INTERNAL STIFFENER AT 11 O'CLOCK FWD MOST HOLE IS CRACKED. CUT AND REMOVED THE DAMAGE PART OF THE INLET INTERNAL STIFFENER. FABRICATED A REPAIR ANGLE, APPROXIMATELY 3.5" LONG AND INSTALLED ANGLE.
- [SDR VNAA201411170006](https://openairdocs.org/sdr/VNAA201411170006.md): Stringer · cracked · Nov 17, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED.750' LONG AT BS 379.
- [SDR VNAA2014111700005](https://openairdocs.org/sdr/VNAA2014111700005.md): Bulkhead · cracked · Nov 17, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 HAS EVIDENCE OF CRACK ON FWD AND AFT SIDE OF BULKHEAD AROUND PARKING BRAKE CABLE HOLE.
- [SDR VNAA2014100200002](https://openairdocs.org/sdr/VNAA2014100200002.md): Target · out of rig · Oct 2, 2014 · N254PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE WARNING MESSAGE DURING FLIGHT. LEFT GEAR SHOWED DASHES. MANUAL RELEASE WORKED NORMALLY. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND PROXIMITY SENSOR ELECTRONIC UNIT FLAGGING LEFT LANDING GEAR UP
- [SDR VNAA2014061500013](https://openairdocs.org/sdr/VNAA2014061500013.md): Carbon Seal · leaking · Jun 15, 2014 · N254PS · Cndair CL6002B19 · AC Generator-Alternator
  > CREW REPORTED LT ENGINE OIL PRESSURE RED WARNING MESSAGE AT FL320. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND IDG CARBON SEAL LEAKING. MAINTENANCE R & R LT ENGINE IDG CARBON SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR
- [SDR VNAA2014051500009](https://openairdocs.org/sdr/VNAA2014051500009.md): Structure · damaged · May 15, 2014 · N254PS · Cndair CL6002B19 · Fuselage Structure (General)
  > CREW REPORTED POSSIBLE LIGHTNING STRIKE ON LT SIDE OF ACFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R THE LOWER VHF ANTENNA AND STATIC WICKS ON HORIZONTAL STABILIZER. REPAIR PERFORMED FOR BURN MARK ON LT SIDE AFT TAIL CONE. MAINTENANCE PER
- [SDR VNAA2014020400002](https://openairdocs.org/sdr/VNAA2014020400002.md): Feeder Cable · damaged · Feb 4, 2014 · N254PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT POWER STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N254PS-2025-12-09/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N254PS' AND deregistration_id = 'N254PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N254PS-2025-12-09/reports

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